What's the initialization method in FINE/turbo?
As the title says, when we set the Fine/turbo solver init, there's a selection of "for turbomachinery", and we shoud give a pressure.
But I'm not quite understand what it means.
The general rotation speed of a compressor rotor is about 17000rpm. Very fast right? How can the solver guarantee the Convergence? I think the initial method is very important.
Is there anybody familiar with it?
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